CA2034466A1 - Stratoreacteur a cycle de combustion ameliore - Google Patents
Stratoreacteur a cycle de combustion amelioreInfo
- Publication number
- CA2034466A1 CA2034466A1 CA002034466A CA2034466A CA2034466A1 CA 2034466 A1 CA2034466 A1 CA 2034466A1 CA 002034466 A CA002034466 A CA 002034466A CA 2034466 A CA2034466 A CA 2034466A CA 2034466 A1 CA2034466 A1 CA 2034466A1
- Authority
- CA
- Canada
- Prior art keywords
- fuel
- combustor
- airflow
- generating
- inlet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000002485 combustion reaction Methods 0.000 title abstract description 7
- 239000000446 fuel Substances 0.000 claims abstract description 61
- 239000000203 mixture Substances 0.000 claims abstract description 39
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 37
- 238000000034 method Methods 0.000 claims abstract description 29
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 22
- 239000001301 oxygen Substances 0.000 claims abstract description 21
- 239000000567 combustion gas Substances 0.000 claims abstract description 16
- 238000006243 chemical reaction Methods 0.000 claims abstract description 13
- 230000006798 recombination Effects 0.000 claims abstract description 13
- 238000005215 recombination Methods 0.000 claims abstract description 13
- 230000002269 spontaneous effect Effects 0.000 claims abstract description 13
- 230000005465 channeling Effects 0.000 claims abstract description 7
- 238000010494 dissociation reaction Methods 0.000 claims description 5
- 230000005593 dissociations Effects 0.000 claims description 5
- 230000003068 static effect Effects 0.000 claims description 5
- 238000007599 discharging Methods 0.000 claims description 4
- 238000011144 upstream manufacturing Methods 0.000 claims 7
- UFHFLCQGNIYNRP-VVKOMZTBSA-N Dideuterium Chemical compound [2H][2H] UFHFLCQGNIYNRP-VVKOMZTBSA-N 0.000 claims 2
- YZCKVEUIGOORGS-UHFFFAOYSA-N Hydrogen atom Chemical compound [H] YZCKVEUIGOORGS-UHFFFAOYSA-N 0.000 claims 2
- 208000037656 Respiratory Sounds Diseases 0.000 description 11
- 206010037833 rales Diseases 0.000 description 11
- 239000007789 gas Substances 0.000 description 10
- 230000035939 shock Effects 0.000 description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 4
- 230000014509 gene expression Effects 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 101100075096 Drosophila melanogaster lolal gene Proteins 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 241000180579 Arca Species 0.000 description 1
- NLZUEZXRPGMBCV-UHFFFAOYSA-N Butylhydroxytoluene Chemical compound CC1=CC(C(C)(C)C)=C(O)C(C(C)(C)C)=C1 NLZUEZXRPGMBCV-UHFFFAOYSA-N 0.000 description 1
- 101710128746 Cytochrome b6-f complex iron-sulfur subunit 1 Proteins 0.000 description 1
- 241000288140 Gruiformes Species 0.000 description 1
- 101100238304 Mus musculus Morc1 gene Proteins 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 241000894007 species Species 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/471,332 US5058826A (en) | 1990-01-29 | 1990-01-29 | Scramjet engine having a low pressure combustion cycle |
| US471,332 | 1990-01-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2034466A1 true CA2034466A1 (fr) | 1991-07-30 |
Family
ID=23871219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002034466A Abandoned CA2034466A1 (fr) | 1990-01-29 | 1991-01-17 | Stratoreacteur a cycle de combustion ameliore |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US5058826A (fr) |
| CA (1) | CA2034466A1 (fr) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5202525A (en) * | 1990-01-29 | 1993-04-13 | General Electric Company | Scramjet engine having improved fuel/air mixing |
| US5255513A (en) * | 1990-02-28 | 1993-10-26 | General Electric Company | Method of operating a scramjet including integrated inlet and combustor |
| GB2267733A (en) * | 1992-05-13 | 1993-12-15 | Gen Electric | Abrasion protective and thermal dissipative coating for jet engine component leading edges. |
| US5372005A (en) * | 1992-09-14 | 1994-12-13 | Lawler; Shawn P. | Method and apparatus for power generation |
| US5709076A (en) * | 1992-09-14 | 1998-01-20 | Lawlor; Shawn P. | Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall |
| US5317866A (en) * | 1992-09-18 | 1994-06-07 | Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government | Free-flying tubular vehicle |
| US5513571A (en) * | 1994-05-17 | 1996-05-07 | Rockwell International Corporation | Airbreathing propulsion assisted gun-launched projectiles |
| US5485787A (en) * | 1994-06-21 | 1996-01-23 | Rockwell International Corporation | Gas gun launched scramjet test projectile |
| CN1092289C (zh) | 1996-12-16 | 2002-10-09 | 拉姆金动力系统公司 | 产生动力用的冲压喷射发动机 |
| ZA993917B (en) | 1998-06-17 | 2000-01-10 | Ramgen Power Systems Inc | Ramjet engine for power generation. |
| AUPQ361299A0 (en) * | 1999-10-22 | 1999-11-18 | University Of Queensland, The | Reducing skin friction drag |
| CN1318748C (zh) * | 2003-10-31 | 2007-05-30 | 王德强 | 一种超燃冲压发动机 |
| US7516918B2 (en) * | 2006-05-11 | 2009-04-14 | The Boeing Company | Morphable ceramic composite skins and structures for hypersonic flight |
| US20100155357A1 (en) * | 2006-06-12 | 2010-06-24 | The Clorox Company | Liner Material |
| US20070286978A1 (en) * | 2006-06-12 | 2007-12-13 | Dennis Stephen R | Liner material |
| JP5758160B2 (ja) * | 2011-03-23 | 2015-08-05 | 三菱重工業株式会社 | スクラムジェットエンジン |
| JP2016056692A (ja) * | 2014-09-05 | 2016-04-21 | 国立大学法人東北大学 | スクラムジェットエンジン用燃焼装置及びスクラムジェットエンジン |
| US10794331B2 (en) * | 2017-07-31 | 2020-10-06 | The Boeing Company | Scramjets and associated aircraft and methods |
| JP7001489B2 (ja) | 2018-02-09 | 2022-01-19 | 三菱重工業株式会社 | スクラムジェットエンジン及び飛翔体 |
| CN109896022B (zh) * | 2019-03-28 | 2023-12-08 | 河南机电职业学院 | 一种轻型无人机高压气动助推起飞装置 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3783616A (en) * | 1961-03-02 | 1974-01-08 | Garrett Corp | Control method for detonation combustion engines |
| US3407603A (en) * | 1961-07-27 | 1968-10-29 | Garrett Corp | Reaction propulsion engines |
| US3280565A (en) * | 1963-01-10 | 1966-10-25 | Gordon L Dugger | External expansion ramjet engine |
| US3430446A (en) * | 1964-04-20 | 1969-03-04 | Us Navy | External burning ramjet engine |
| US4194519A (en) * | 1964-11-18 | 1980-03-25 | The United States Of America As Represented By The Secretary Of The Navy | Hypersonic modular inlet |
| US3535882A (en) * | 1966-12-27 | 1970-10-27 | Fairchild Hiller Corp | Scramjet aircraft |
| US4214442A (en) * | 1968-08-08 | 1980-07-29 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Combustion chambers operating on a supersonic stream chiefly for jet engines |
| US3974648A (en) * | 1968-08-19 | 1976-08-17 | United Technologies Corporation | Variable geometry ramjet engine |
| GB1605304A (en) * | 1976-08-17 | 1988-10-05 | Rolls Royce | Rockets |
| US4369940A (en) * | 1979-12-17 | 1983-01-25 | Mcdonnell Douglas Corporation | Airbreathing propulsion system for supersonic vehicles |
| US4381017A (en) * | 1980-04-05 | 1983-04-26 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Air inlet, especially a two-dimensional air inlet set at an angle on one side for gas turbine jet propulsion plants for driving airplanes |
| US4477039A (en) * | 1982-06-30 | 1984-10-16 | Mcdonnell Douglas Corporation | Vented cowl variable geometry inlet for aircraft |
| US4817892A (en) * | 1986-04-28 | 1989-04-04 | Janeke Charl E | Aerospace plane and engine therefor |
| US4821512A (en) * | 1987-05-05 | 1989-04-18 | United Technologies Corporation | Piloting igniter for supersonic combustor |
-
1990
- 1990-01-29 US US07/471,332 patent/US5058826A/en not_active Expired - Fee Related
-
1991
- 1991-01-17 CA CA002034466A patent/CA2034466A1/fr not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| US5058826A (en) | 1991-10-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2034466A1 (fr) | Stratoreacteur a cycle de combustion ameliore | |
| US4206593A (en) | Gas turbine | |
| US6062018A (en) | Pulse detonation electrical power generation apparatus with water injection | |
| CN1784574B (zh) | 截流涡流式燃烧器 | |
| EP3622218B1 (fr) | Système d'échangeur de chaleur à combustion par impulsions | |
| US20110302908A1 (en) | Multitube valveless pulse detonation engine | |
| AU2016382619A1 (en) | Micro-turbine gas generator and propulsive system | |
| EA200501731A1 (ru) | Камера сгорания (варианты) и способ использования камеры сгорания | |
| CN111594346A (zh) | 一种中等尺度火箭基组合循环发动机 | |
| CA1313457C (fr) | Compresseur pour moteur a reaction | |
| GB1329944A (en) | Mounting of fuel injection manifolds in combustion chambers | |
| US5333445A (en) | Scramjet engine having improved fuel/air mixing | |
| JPS6355350A (ja) | パルス・ジェット・ノズル | |
| KR101616647B1 (ko) | 직사각형단면을 가지는 극초음속 공기 흡입식 복합 사이클 엔진 | |
| US3382679A (en) | Jet engine with vaporized liquid feedback | |
| US3516253A (en) | Combustion system for producing high temperature and high pressure gas | |
| Sislian | Detonation-wave ramjets | |
| US3488952A (en) | Apparatus for alternatively supplying combustion products and cooling air to separate turbine wheels | |
| US3365880A (en) | Combustion apparatus for producing a high kinetic energy working gas stream and method of its use | |
| US2998705A (en) | Pressure gain valveless combustior | |
| US4896501A (en) | Turbojet engine with sonic injection afterburner | |
| CN111594347A (zh) | 一种大尺度多级火箭基组合循环发动机 | |
| CN1611761A (zh) | 一种超燃冲压发动机 | |
| CN1472433A (zh) | 射流增压式推力可控脉冲爆轰发动机及提高其推力的方法 | |
| Schadow et al. | Water tunnel and windowed combustion as tools for ducted rocket development |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |